The readers are referred to Adhikari and Bhattacharya (2010), Bhattacharya and Adhikari (2011), and Arany et al. (2015a,b, 2016, 2017) for comprehensive understanding. The fundamentals are provided here.
The equation of motion using the Euler‐Bernoulli beam model for a beam with an axial force is
where EI(z) is the bending stiffness distribution along the axial coordinate z, μ(z) is the distribution of mass per unit length, P* is the axial force acting on the beam due to the top head mass and the self‐weight of the tower, p(z, t) is the excitation of the beam, w(z, t) is the deflection profile.
Using constant equivalent values for the axial force, bending stiffness and mass per length, and considering free harmonic vibration of the beam with separation of variables w(z, t) = W(z) · eiωt, the equation can be reduced to the following using the non‐dimensional parameters of Table B.1 and the dimensionless axial coordinate ξ = z/L:
Table B.1 Nondimensional variables.
Dimensionless group | Formula | Dimensionless group | Formula |
Nondimensional lateral stiffness | ![]() |
Nondimensional axial force | ![]() |
Nondimensional rotational stiffness | ![]() |
Mass ratio | ![]() |
Nondimensional cross stiffness | ![]() |
Nondimensional rotary inertia | ![]() |
KL, KR, KLR are the lateral, rotational, and cross stiffness of the foundation, respectively; EIη is the equivalent bending stiffness of the tapered tower; LT is the hub height above the bottom of the tower; P* is the modified axial force, mRNA is the mass of the rotor‐nacelle assembly; mT is the mass of the tower; J is the rotary inertia of the top mass; μ is the equivalent mass per unit length of the tower.
where is the nondimensional axial force and
is the non‐dimensional circular frequency).
Using the nondimensional numbers as defined above, the boundary conditions can be written for the bottom of the tower (ξ = 0):
and the top of the tower (ξ = 1):
The parameters used in the boundary conditions are defined in Table B.1. The characteristic equation for the equation of motion can be written as
and
The four solutions are then
with which the solution is in the form
which can be transformed using Euler's identity to
with
Substituting this form of the solution into the boundary conditions, one obtains four equations, written in matrix form as
with
and
Looking for nontrivial solutions of this equation one obtains
from which one can obtain the nondimensional circular frequency Ω, and from that the natural frequency using
The equation that has to be solved is transcendental and therefore solutions can only be obtained numerically.
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